# Service difficulty reports: N765SA, cancelled Dec 23, 2015

A list on [N765SA, cancelled Dec 23, 2015](https://openairdocs.org/deregistered/N765SA-2015-12-23.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR Q2SA2012080876504](https://openairdocs.org/sdr/Q2SA2012080876504.md): Case · cracked · Aug 8, 2012 · N765SA · Boeing 7472F6B · Engine (Turbine/Turboprop)
  > NORMAL FLAPS 20 TAKEOFF WITH REDUCED THRUST. AT 1000 AGL, NR 3 FIRE WARNING ILLUMINATED AND FIRE BELL SOUNDED. SHUTDOWN ENGINE PER QRH PROCEDURES. REQUESTED AND RECEIVED VECTORS TO DUMP FUEL OVER THE WATER, DUMPED DOWN TO MAKE 630 LANDING WEIGHT. AFTER ENGI
- [SDR Q2SA20111211001](https://openairdocs.org/sdr/Q2SA20111211001.md): Hydraulic Line · chafed · Dec 11, 2011 · N765SA · Boeing 7472F6B · Hydraulic System, Main
  > APPROXIMATELY ONE HOUR INTO FLIGHT, NUMBER FOUR HYDRAULIC QUANTITY DROPPED TO 2.4 GALLONS. FOLLOWED QRH PROCEDURES BY TURNING PUMPS OFF. FINISHED QRH PRIOR TO LANDING. FOUND NR 4 HYDRAULIC RETURN LINE LEAKING. REPLACED NR 4 HYDRAULIC RETURN LINE IAW B747-A
- [SDR Q2SA765002](https://openairdocs.org/sdr/Q2SA765002.md): Sense Line · loose · Sep 16, 2011 · N765SA · Boeing 7472F6B · Pneumatic Indicating System
  > ON 09/16/11, ETH 3718 FROM HAAB TO VHHH - APPROXIMATELY 15 MINUTES AFTER TAKEOFF, CLIMBING THROUGH FL 170, NUMBER FOUR ENGINE FIRE WARNING ANNUNCIATED. THE CREW ACCOMPLISHED ALL MEMORY ITEMS, DECLARED AN EMERGENCY AND COORDINATED WITH ATC TO RETURN TO ADDIS.
- [SDR TX9Y20110823001](https://openairdocs.org/sdr/TX9Y20110823001.md): Skin Panel · corroded · Aug 22, 2011 · N765SA · Boeing 747200F · Wing, Plate/Skin
  > LT WING / STA WS 1295 / LT OUTER WING LOWER SKIN PANEL LOWER SURFACE AROUND MID SPAR FASTENER HOLES FOUND CORROSION.
- [SDR TX9Y20110819007](https://openairdocs.org/sdr/TX9Y20110819007.md): Floorbeam · corroded · Aug 18, 2011 · N765SA · Boeing 747200F · Fuselage Main, Floor Beam
  > FORWARD CARGO / STA BS 760 / FLOORBEAM UPPER CHORD FOUND CORROSION.
- [SDR TX9Y20110819006](https://openairdocs.org/sdr/TX9Y20110819006.md): Floorbeam · corroded · Aug 18, 2011 · N765SA · Boeing 747200F · Fuselage Main, Floor Beam
  > FORWARD CARGO / STA BS 740RT / FLOORBEAM UPPER CHORD FOUND CORROSION.
- [SDR TX9Y20110819005](https://openairdocs.org/sdr/TX9Y20110819005.md): Skin · corroded · Aug 18, 2011 · N765SA · Boeing 747200F · Fuselage Main, Plate/Skin
  > FUSELAGE / STA BS 2160 BETWEEN STR 46R-47R / SKIN FOUND CORROSION.
- [SDR TX9Y20110819004](https://openairdocs.org/sdr/TX9Y20110819004.md): Skin · corroded · Aug 18, 2011 · N765SA · Boeing 747200F · Wing, Plate/Skin
  > LT WING / STA WBL 130-140 / UPPER REAR AREA FOUND CORROSION.
- [SDR TX9Y20110819003](https://openairdocs.org/sdr/TX9Y20110819003.md): Stringer · corroded · Aug 18, 2011 · N765SA · Boeing 747200F · Fuselage Main, Longeron/Stringer
  > BULK CARGO / STA BS 2160 STR 48L / STRINGER FOUND CORROSION.
- [SDR TX9Y20110819002](https://openairdocs.org/sdr/TX9Y20110819002.md): Stringer · corroded · Aug 18, 2011 · N765SA · Boeing 747200F · Fuselage Main, Longeron/Stringer
  > BULK CARGO / STA BS 2160 STR 47L / STRINGER FOUND CORROSION.
- [SDR TX9Y20110819001](https://openairdocs.org/sdr/TX9Y20110819001.md): Skin · corroded · Aug 18, 2011 · N765SA · Boeing 747200F · Fuselage Main, Plate/Skin
  > FUSELAGE / STA BS 1900-1920 STR 46R/ LAP SKIN FOUND CORROSION.
- [SDR WGFY2010FA0000494](https://openairdocs.org/sdr/WGFY2010FA0000494.md): Stiffener · cracked · Jun 30, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Main Frame
  > PYLON NR1 STIFFENER NR3 BETWEEN NAC STA 234-259 WAS CRACK +/- 25MM. PERFORMED A DETAIL VISUAL REPEAT INSPECTION OF SUBJECT REPAIR AREA AT THE INSPECTION INTERVAL SPECIFICATION IN THE SB 747-54-2223 TO ENSURE ABSENCE OF ANY ADDITIONAL HEAT DAMAGE, LOOSE FAST
- [SDR WGFY2010FA0000496](https://openairdocs.org/sdr/WGFY2010FA0000496.md): Stringer · corroded · Jun 30, 2010 · N765SA · Boeing 7472F6B · Fuselage Main, Longeron/Stringer
  > STRINGER 43 LT WAS CORROSION STA 960-1000 AT BELOW FWD CARGO AREA. REPAIR CLASSIFICATION FOR SRM REPAIR: CAT 'B', REPETITIVE INSP SRM 53-10-03 FIG 1, SHEET 6, TABLE IV. SRM 51-10-06, 51-21-00, 53-10-03 FIG 1, 51-10-02. REPAIR REPETITIVE INSPECTION REQUIREME
- [SDR WGFY2010FA0000493](https://openairdocs.org/sdr/WGFY2010FA0000493.md): Skin · corroded · Jun 30, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/Skin
  > PYLON NR 3 UPPER DSB LOWER WING SKIN WAS CORROSION LEVEL 2.
- [SDR WGFY2010FA0000489](https://openairdocs.org/sdr/WGFY2010FA0000489.md): Skin · corroded · Jun 30, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/Skin
  > (WGFY) PYLON NR 4 UPPER DSB LOWER WING SKIN WAS CORROSION LEVEL 2, REFER TO JOB CARDS NR 54-812-01-04. MFG MESSAGE: YDK-SOF-10-0011-04B/18 MAY 2010, YDK-SOF-10-0011-09B/03 JUNE 2010, YDK-SOF-10-0011-11B/05JUNE 2010. PERFORM REPEAT DVI INSPECTION OF THE SU
- [SDR WGFY2010FA0000488](https://openairdocs.org/sdr/WGFY2010FA0000488.md): Skin · corroded · Jun 29, 2010 · N765SA · Boeing 7472F6B · Wing, Plate/Skin
  > PYLON NR2 LT WING LOWER FRONT SPAR LOWER WING SKIN WBL 470 WAS CORRODED LEVEL 2,
- [SDR WGFY2010FA0765014](https://openairdocs.org/sdr/WGFY2010FA0765014.md): Skin · delaminated · Jun 3, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/Skin
  > ((WGFY)) PYLON NR 3 LT INNER SKIN DELAMINATION (BETWEEN NAC STA 201.60 TO 240.00) PERFORMED DVI OF THE REPAIR ZONE AT THE REPEAT "C" CHECK, PERFORM REPEAT DVI INSPECTION PER SB 747 54A2182R2 REQUIREMENT AT 1200 FLIGHT CYCLE INTERVAL NOT TO EXCEED 24 MOUNTHS
- [SDR WGFY2010FA0765013](https://openairdocs.org/sdr/WGFY2010FA0765013.md): Skin · corroded · Jun 3, 2010 · N765SA · Boeing 7472F6B · Wing, Plate/Skin
  > ((WGFY)) THERE IS GAP L=2.73 INCH. W=0.78 INCH.T=0.029 BETWEEN LT LOWER SURFACE AND UNDER WING FUSE PIN FITTING PYLON NR 1 WING STA 116.8. PERFORMED A DETAIL VISUAL INSPECTION OF THE REPAIR ZONE, C-CHECK PERFORMED REPEAT DVI INSPECTION OF THE SUBJECT AREA I
- [SDR WGFY2010FA0765011](https://openairdocs.org/sdr/WGFY2010FA0765011.md): Skin · delaminated · Jun 2, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/Skin
  > ((WGFY)) PYLON NR 2, SKIN PYLON NR 2 DELAMINATION (RT INNER SIDE) BETWEEN NAC 201,4 TO NAC STA 286,00. PERFORM A REPEATED DVI OF THE SUBJECT REPAIRED AREAS AT EVERY "C" CHECK OR 18 MONTHS, WHICH EVER OCCURS FIRST.
- [SDR 2010F00120](https://openairdocs.org/sdr/2010F00120.md): Skin · delaminated · Jun 2, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/Skin
  > PYLON NR2, SKIN PYLON NR2 DELAMINATION ( RT INNER SIDE) BETWEEN NAC STA 201.4 TO NAC STA 286,00.
- [SDR 2010F00119](https://openairdocs.org/sdr/2010F00119.md): Skin · delaminated · Jun 2, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/Skin
  > PYLON NR 2, SKIN PYLON NR 2 DELAMINATION ( RT INNER SIDE)BETWEEN NAC STA 201.4 TO NAC STA 286,00.
- [SDR WGFY2010FA0000495](https://openairdocs.org/sdr/WGFY2010FA0000495.md): Stiffener · cracked · May 25, 2010 · N765SA · Boeing 7472F6B · Fuselage Miscellaneous Structure
  > FUSELAGE RT SIDE VERTICAL STIFFENER STA 980, RBL 11,33 WAS CRACKED AND PERFORM HFEC INSPECTION METHOD TO ENSURE CRACK:+/- 20MM. REPLACED VERTICAL STIFFENER IAW SRM 51-30-02 PART 116.
- [SDR 2010FA0000496](https://openairdocs.org/sdr/2010FA0000496.md): Stringer · corroded · May 20, 2010 · N765SA · Boeing 7472F6B · Fuselage Main, Longeron/Stringer
  > STRINGER 43 LT CORRODED STA 960-1000 AT AREA BELOW FORWARD CARGO.
- [SDR 2010FA0000495](https://openairdocs.org/sdr/2010FA0000495.md): Stiffener · cracked · May 20, 2010 · N765SA · Boeing 7472F6B · Fuselage Miscellaneous Structure
  > FUSELAGE RT SIDE VERTICAL STIFFENER STA.980, RBL 11,33 WAS CRACKED AND PERFORM HFEC INSPECTION METHOD TO ENSURE CRACK:+/- 20MM
- [SDR 2010FA0000494](https://openairdocs.org/sdr/2010FA0000494.md): Stiffener · cracked · May 20, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION:PYLON NR 1 STIFFENER NR 3 BEWEEN NAC STA.234-259 WAS CRACK +/- 25MM
- [SDR 2010FA0000493](https://openairdocs.org/sdr/2010FA0000493.md): Skin · corroded · May 20, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/Skin
  > PYLON NR 3 UPPER DSB LOWER WING SKIN WAS CORROSION LEVEL 2
- [SDR 2010FA0000489](https://openairdocs.org/sdr/2010FA0000489.md): Skin · corroded · May 19, 2010 · N765SA · Boeing 7472F6B · Wing, Plate/Skin
  > PYLON NR 4 UPPER DSB LOWER WING SKIN WAS CORROTION LEVEL 2, REFER TO JOB CARDS NR 54-812-01-04.
- [SDR 2010FA0000488](https://openairdocs.org/sdr/2010FA0000488.md): Skin · corroded · May 19, 2010 · N765SA · Boeing 7472F6B · Wing, Plate/Skin
  > PYLON NR 2 LT WING LOWER FRONT SPAR LOWER WING SKIN WBL 470 WAS CORROTION LEVEL 2, REFER TO JOB CARDS 57-216-02-01.
- [SDR 2010FA0000487](https://openairdocs.org/sdr/2010FA0000487.md): Skin · cracked · May 19, 2010 · N765SA · Boeing 7472F6B · Fuselage Main, Plate/Skin
  > EAO 4753070 R1,FUSELAGE-CENTER SECTION -BODY STATION 1480 BULKHEAD AND SPLICE COMPONENT INSPECTION REPAIR AND MODIFICATION,HFEC INSPECT FOUND HOLE NR 3 OF LONGERON EXTENSION FITTING SKIN PANEL CRACK
- [SDR 2010FA0000486](https://openairdocs.org/sdr/2010FA0000486.md): Stringer · corroded · May 19, 2010 · N765SA · Boeing 7472F6B · Fuselage Main, Longeron/Stringer
  > STRINGER 43 LT CORRODED AT STA 960 TO STA 1000 AREA BELOW FORWARD CARGO
- [SDR 2010FA0000485](https://openairdocs.org/sdr/2010FA0000485.md): Stiffener · cracked · May 18, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon Miscellaneous Structure
  > PYLON NR 1 STIFFENER NR 3 BETWEEN NAC STA.234-259 WAS CRACK +/- 25MM
- [SDR Q2SA765001](https://openairdocs.org/sdr/Q2SA765001.md): Duct · ruptured · Nov 2, 2009 · N765SA · Boeing 7472F6B · Engine Bleed Air System
  > ON TAKEOFF ROLL OUT OF VHHH ENGINE NR 4 HAD EXHAUST GAS TEMPERATURE OVERTEMP AS WELL AS NACELLE TEMPERATURE RISE. CREW CONTINUED TAKE OFF SUCCESSFULLY BUT ELECTED TO TERMINATE FLIGHT, DUMPED 137,000 LBS OF FUEL, RETURNED AND LANDED SAFELY AT VHHH. AFTER LAND

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N765SA' AND deregistration_id = 'N765SA-2015-12-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N765SA-2015-12-23/reports

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